EP0227131B1 - Objet laminé comprenant des feuilles de fibres métalliques - Google Patents
Objet laminé comprenant des feuilles de fibres métalliques Download PDFInfo
- Publication number
- EP0227131B1 EP0227131B1 EP86201928A EP86201928A EP0227131B1 EP 0227131 B1 EP0227131 B1 EP 0227131B1 EP 86201928 A EP86201928 A EP 86201928A EP 86201928 A EP86201928 A EP 86201928A EP 0227131 B1 EP0227131 B1 EP 0227131B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- fibres
- web
- active
- fibre
- mixed
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/12—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/002—Manufacture of articles essentially made from metallic fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/02—Layer formed of wires, e.g. mesh
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/20—Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/12—Radiant burners
- F23D14/16—Radiant burners using permeable blocks
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/103—Metal fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/14—Mixture of at least two fibres made of different materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/80—Sintered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C2204/00—End product comprising different layers, coatings or parts of cermet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2203/00—Gaseous fuel burners
- F23D2203/10—Flame diffusing means
- F23D2203/105—Porous plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2203/00—Gaseous fuel burners
- F23D2203/10—Flame diffusing means
- F23D2203/107—Flame diffusing means coated with catalysts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2212/00—Burner material specifications
- F23D2212/20—Burner material specifications metallic
- F23D2212/201—Fibres
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12035—Fiber, asbestos, or cellulose in or next to particulate component
Definitions
- the invention relates to laminated porous objects comprising various layers of metal fibre webs that are bonded together in the interfaces by a sintering operation, the metal fibre composition differing in at least two adjacent layers.
- metal fibre webs the fibre diameter in one layer differing from the fibre diameter in the adjacent layer or layers.
- Such metal fibre webs are, e.g. described in British Patent 1,190,844, which also specifies a method of forming metal fibres through bundled drawing.
- a pronounced resistance is required, be it to high temperature, to fluctuations of temperature, to abrasion, to oxidation or to other chemical corrosion or physical or mechanical disintegration.
- the invention provides a laminated object of metal fibre webs sintered on top of each other wherein at least one web comprises active fibres and which web is adjacent to a mixed-fibre web comprising a mixture of the active fibres and other metal fibres which can be attached to the active fibres by a sintering operation.
- the mixed-fibre web will often act as intermediate layer between a web of active fibres and a carrier or support whereto it can be joined or attached by e.g. sintering or brazing or adhering.
- the support can e.g. be a network or a sheet or plate.
- the support itself can also totally or partly consist of a metal fibre web in contact with the mixed-fibre web.
- the metal fibres in the support web will then preferably be the same as the other (non-active) metal fibres in the mixed-fibre web. Thus, they will be able to form a firm bond with these other fibers as they are attached together by sintering.
- the laminated and sintered porous combination of active-fibre web, mixed-fibre web and support web forms a structure which easily lends itself to further processing, handling and deformation (bending, folding, welding), mechanical damage of the active-fibre web (through breaking or tearing during treatment) being prevented.
- the mixed-fibre web constitutes a key element of the invention as compatible bridge connection between active fibres and the other layers in the laminated object.
- the total weight of the mixed-fibre web will have to amount to at least approximately 50 g/m 2.
- a practically equal quantity by weight of active fibres and non-active fibres will implyy be incorporated in the mixed-fibre web although the proportion can be freely adjusted in accordance with specific bonding requirements between active fibre web and support.
- the mixed-fibre web is to have a total weight of at least 150 g/m 2 it can be composed of a number of thin layers of approximately from 50 to 100 g/m 2 each, by alternately applying layers of active fibres and layers of non-active fibres. Indeed, these layers are thin and highly porous so that when compacting and sintering the built-up stack, the fibres of one layer penetrate to some extent between the fibres of each adjacent layer thus creating a certain mixture.
- This laminated structure of very thin webs is also regarded as being an embodiment of a mixed-fibre web (hence covered by the concept of mixed-fibre web in accordance with the invention).
- mixed-fibre webs having a concentration gradient of active fibres through their thickness.
- the highest concentration (weight ratio) of active fibres will then be chosen in the mixed-fibre web surface that is to constitute the contact or boundary layer interface with the web of active fibres (that is) to be joined to it.
- the concentration at this contact layer will e.g. be approximately 75%.
- the mixed-fibre web with concentration gradient will in face be composed of a number of superposed mixed-fibre sub-webs comprising mutually different active-fibre concentrations.
- a three-layer structure can be made up of active-fibre concentrations of 75, 50 and 25 wt. pct. respectively.
- Each sub-web will then weigh at least 50 g/m 2 and the sub-webs can be cross-laid if desired. This entails that the orientation of a sub-web (i.e. the direction wherewith it leaves the web forming machine) in the mixed-fibre laminate differs from that of an adjacent sub-web.
- This concentration gradient procures a gradual transition between active and non-active fibres thus efficiently and durably preventing a delamination tendency in the interfaces and inside the intermediate layer upon repeated folding or due to mechanical or thermal shocks.
- a portion of the non-active fibres in the mixed-fibre webs can be intended only as non-active filling having e.g. some reinforcing effect.
- Active and non-active fibres in the mixed-fibre webs can furthermore at least partly differ in diameter. This way, a bridge can be established, if desired, between a layer of fine active fibres on the one side and a layer of coarser fibres in the support web or network on the other side. Further, a concentration gradient can be established over more than two fibre types.
- the mixed-fibre web adjacent to the active-fibre layer comprising 50% active fibres, 25% less active fibres and 25% non-active fibres.
- a mixed-fibre web can be joined thereunto with 50% less active fibres and 50% non-active fibres and, subsequently, a mixed-fibre web with 25% less active fibres and 75% non-active fibres.
- the mixed-fibre web can constitute an intermediate layer joining two layers of active fibres which can be joined to the intermediate layer by sintering.
- the active fibres in the one layer can either be the same as or be different from the active fibres in the layer on the opposite side of the mixed-fibre web.
- the structure and composition of the mixed-fibre web or sub-webs can be freely adjusted through a modification in the dosage of active and non-active fibres during the formation of the mixed- webs. For this embodiment it can even be considered to interpose between two mixed-fibre sub-webs some rigid or supple sheet partition, network, honeycomb structure that can be joined and attached to the sub-webs.
- Another embodiment relates to covering both sides of one or more layers of active fibres with a mixed-fibre web.
- This laminated structure can be covered further, at least in part, with materials that can be bonded to the respective surfaces of the two mixed-fibre webs.
- the structure or concentration gradient in the mixed-fibre webs can of course be freely adjusted.
- a laminated structure containing centrally situated mixed webs enclosed between two layers of active fibres will be able to act as joining layer between layers than can be bonded to these active-fibre layers.
- An important field of application of the invention relates to the use of laminated objects wherein active fibres are incorporated that are resistant to high-temperature oxidation.
- Such fibres can be manufactured by methods of bundle drawing known in the art, as described e.g. in U.S. Patents 2,050,298; 3,277,564 or 3,394,213.
- numerous alloy compositions are known, by themselves meeting these conditions of oxidation resistance, e.g. alloys with a base of Fe/NUCo-Cr-AI whether or not with small additions of Y, rare earths or Si.
- Less, yet still adequately resistant alloys are known under the trade names of Inconel, Haynes, Nimonic, Hastelloy and Nichrome.
- These fibres can e.g. be utilised in sintered web form as radiation membrane in radiant burners for liquid or gaseous fuels, the active, oxidation resistant fibres being situated on the outside, i.e. the radiant side of the membrane in the burner.
- the radiation membrane will preferably have a porosity of between 65% and 90%.
- the radiant membrane can be executed as a flat structure which shuts off the supply chamber of gas (e.g. natural gas) or liquid (e.g. fuel oils, diesel oil or petrol) to be combusted at its downstream end.
- gas e.g. natural gas
- liquid e.g. fuel oils, diesel oil or petrol
- the laminated membrane will then according to the invention be composed of a sintered fibre web of e.g.
- Fe-Cr-AI-Y-fibres with a fibre diameter of between 4 and 50 11m on the radiant side of the burner.
- this thin surface layer will have a thickness of e.g. I to 2 mm and will upstream (fuel flow) be bonded by sintering to a mixed-fibre web of e.g. 150 g/m 2 comprising approximately 50 wt. pct. of the Fe-Cr-AI-Y-fibres and 50 wt. pct. stainless steel fibres and/or Inconel fibres.
- a web of stainless fibres (AISI 300 or 400 series, 4-50 1 1m fibre diameter) will then be bonded to this mixed-fibre web to give, among other things, the required strength to the membrane and to realize the appropriate pressure drop for the fuel flow over the thickness of the membrane so that a stable combustion front is obtained.
- This required pressure drop is in general a function of, among other things, the thickness and permeability of the membrane and of the supply pressure and viscosity of the supplied fuel.
- a membrane porosity of between 75% and 90% has been found to be suitable when the total membrane thickness measures 4 - 5 mm.
- the membrane can also be executed in the shape of a cylinder or beam with a bottom plate at the end of the radiant burner opposite from the fuel-supply side.
- a membrane structure of mixed-fibre webs offers the special advantage of being easily pliable into the desired shape without delaminating, thus retaining its robust character.
- Cone or pyramid- shaped membranes (preferably truncated) can also be considered.
- porous ceramic elements can be efficiently and easily attached to a metal support such as e.g. abradable seals in turbine casings of jet engines.
- a thin layer of metal fibres (that can be joined to the material of the turbine casing by e.g. brazing) is covered with a mixed-fibre web of these metal fibres and of (active) Fe-Cr-AI-Y-fibres whereto is joined a thin web of 100% Fe-Cr-AI-Y-fibres.
- This laminate is sintered and covered on the active-fibre side with ceramic material (e.g. by plasma spraying techniques).
- the laminated object according to the invention acts, consequently, as joining layer between a first (ceramic) material resistant to oxidation at high temperature and a second (metal) material, the active fibres adjacent to the first material also being resistant to oxidation at high temperature.
- Another field of application of the invention relates to porous catalysts or catalyst carriers, wherein at least one web in the laminated object comprises catalytically active fibres. Through suitable mixed-fibre webs as intermediate layers, the catalytically active web can then be joined to a suitable carder material.
- the application of Fe-Cr-Al-Y-alloys in catalyst carriers and coated with e.g. Pt as catalyst is known from U.S. patent 3,920,583.
- the laminated object can be part of porous electrodes applicable in eletrolytic baths or as high-temperature resistant, sound-absorbing structures.
- the laminated object can also be applied as separating membrane when treating mixtures with a liquid phase finely divided in a gas phase or in another liquid phase, e.g. in sheets or as separating fillings in absorption or distillation towers.
- the active fibres will then have to possess a specific humidifying or hydrophylic affinity and/or chemical resistance.
- the portion of active fibres will have a high electrical resistance.
- the porous laminated objects according to the invention can also be applied for heat transfer as in heat pipes or heat exchangers e.g. of the type described in U.S. patent 3,262,190. Magnetic fibres or steel wool can be utilised as active fibres for application in magnetic filtration.
- Burner membranes can also be designed wherein ceramic fibres are blended with e.g. the Fe-Cr-AI-Y-fibres described above to reinforce the porous ceramic fibre layer. Indeed, ceramic fibre structures do not form strong bonds in their contact points upon heating or sintering. The provision however of metallic Fe-Cr-AI-Y-fibres in a blended ar- rangment with the ceramic fibres will create numerous strong metal sinter bonds at the mutual contact points of the metal fibres (resistant to oxydation at high temperature) distributed between the ceramic fibres and hence improve the thermal schock resistance of the composite membrane.
- a mixed web of ceramic fibres and e.g. Fe-Cr-AI-Y-fibres can be attached to a layer of active Fe-Cr-AI-Y-fibres resistant to oxydation at high temperature.
- Active fibres of 22 J.1m diameter and composed of 16% Cr, 4.5% Al, 0.3% Y, 0.3% Si and the rest Fe were made by bundle drawing and were dry-processed into a fibre web in accordance with a method analogous to the one described in the British patent 1,190,844.
- a number of these webs are superposed and joined to a stack of similar fibre webs of AISI 316L stainless steel fibres (22 ⁇ m diameter) as non-active fibre layer. This joining is carried out by inserting between active and stainless steel fibre web stacks a mixed-fibre web with a weight of 150 g/m 2 and with an approximately equal part by weight therein of said active fibres and of the AISI 316L stainless steel fibres as non-active fibres.
- the whole has a weight of 4.5 kg/m 2 and is sintered at 1200 ° C for I hour into a porous sheet with a porosity of 84% and a 4 mm thickness.
- the layer of active fibres in the sintered sheet has a thickness of 1.5 mm and the thickness of the adjacent layer of non-active fibres measures 2.5 mm.
- the sheet can be folded and unfolded quite easily and repeatedly without delamination appearing in the intermediate interface at the mixed-fibre web. This operation is not possible with similar sheets without mixed-fibre web; in other words, when folding repeatedly, delamination occurs between the layer of active fibres and the layer of non-active fibres.
- the sheet edges or rims to be joined in the longitudinal seam of the cylinder are joined by welding.
- a narrow longitudinal strip is removed beforehand from the active-fibre web part near one of the said sheet rims and the other sheet rim is laid with the non-active fibre-web rim in the recess. This lap of both sheet rims can then be easily joined in the usual way by a welding operation.
- the invention is not confined to dry-made laminated objects of metal fibre webs.
- the fibre webs can also be made by a wet lay down process, e.g. analogous to paper-making , a suspension of the fibres in a liquid being precipitated onto a filter cloth wherethrough the liquid is drained.
- previously sintered layers of active fibres having a certain porosity can now also be joined by sintering to previously sintered webs of non-active fibres having a porosity or permeability different from that of the layers of active fibres.
- previously sintered mixed-fibre webs inserted are joined by sintering to the other layers, they will be compressed and will form sufficient sintered contact points to realize a tight bond.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
Claims (18)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE1011387 | 1985-11-28 | ||
BE1011387 | 1985-11-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0227131A1 EP0227131A1 (fr) | 1987-07-01 |
EP0227131B1 true EP0227131B1 (fr) | 1990-05-23 |
Family
ID=3862988
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86201928A Expired - Lifetime EP0227131B1 (fr) | 1985-11-28 | 1986-11-05 | Objet laminé comprenant des feuilles de fibres métalliques |
Country Status (4)
Country | Link |
---|---|
US (1) | US4810587A (fr) |
EP (1) | EP0227131B1 (fr) |
JP (1) | JP2593459B2 (fr) |
DE (1) | DE3671407D1 (fr) |
Families Citing this family (28)
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DE3872868T2 (de) * | 1987-12-29 | 1992-12-03 | Bekaert Sa Nv | Verdichtung eines metallgewebes. |
MY105757A (en) * | 1989-01-23 | 1995-01-30 | Minnesota Mining & Mfg | Metal fiber mat/polymer composite |
US5226210A (en) * | 1989-01-23 | 1993-07-13 | Minnesota Mining And Manufacturing Company | Method of forming metal fiber mat/polymer composite |
US5154160A (en) * | 1991-05-12 | 1992-10-13 | Q Industries Food Equipment Co. | Automated oven with gas-fired radiant heater assembly |
US5364080A (en) * | 1991-10-16 | 1994-11-15 | Combustion Concepts, Inc. | High efficient heat treating and drying apparatus and method |
DE4324644A1 (de) * | 1993-07-22 | 1995-01-26 | Gossler Kg Oscar | Keramisches Verbrennungsträgerelement für Flächenbrenner und Verfahren zu seiner Herstellung |
US5642724A (en) * | 1993-11-29 | 1997-07-01 | Teledyne Industries, Inc. | Fluid mixing systems and gas-fired water heater |
US5431557A (en) * | 1993-12-16 | 1995-07-11 | Teledyne Industries, Inc. | Low NOX gas combustion systems |
JP3687215B2 (ja) * | 1995-09-25 | 2005-08-24 | 新東工業株式会社 | 耐熱金属繊維焼結体の製造方法 |
US6102994A (en) * | 1997-03-20 | 2000-08-15 | Alliedsignal Inc. | Alumina-based hydrophilic antimicrobial coating |
US6435861B1 (en) * | 1997-06-10 | 2002-08-20 | Usf Filtration And Separations Group, Inc. | Gas burner assembly and method of making |
BE1011244A3 (nl) * | 1997-06-30 | 1999-06-01 | Bekaert Sa Nv | Gelaagde buisvormige metaalstructuur. |
WO2000008383A2 (fr) * | 1998-08-04 | 2000-02-17 | Clean Energy Combustion Systems Inc. | Ameliorations apportees a des bruleur a diesel |
DE60113087T2 (de) * | 2000-04-17 | 2006-06-29 | N.V. Bekaert S.A. | Gasbrennermembran |
US6558810B2 (en) * | 2000-09-05 | 2003-05-06 | Paul W. Garbo | Forming sintered metal fiber porous mats |
US20030012676A1 (en) * | 2001-05-29 | 2003-01-16 | Quick Nathaniel R. | Formed membrane and method of making |
US20050053816A1 (en) * | 2002-11-15 | 2005-03-10 | Anuj Bhargava | Burner for combusting the anode exhaust gas stream in a PEM fuel cell power plant |
US20040152028A1 (en) * | 2003-02-05 | 2004-08-05 | Singh Prem C. | Flame-less infrared heater |
WO2005028134A1 (fr) * | 2003-09-23 | 2005-03-31 | N.V. Bekaert S.A. | Fibre metallique comportant plus d'un metal ou d'alliage metallique |
US20090176074A1 (en) * | 2006-05-05 | 2009-07-09 | Meadwestvaco Corporation | Conductive/absorbtive sheet materials with enhanced properties |
CN100460756C (zh) * | 2006-12-27 | 2009-02-11 | 东北大学 | 一种金属纤维-多孔陶瓷介质表面燃烧器 |
US8828325B2 (en) * | 2007-08-31 | 2014-09-09 | Caterpillar Inc. | Exhaust system having catalytically active particulate filter |
EP2411650A1 (fr) | 2009-03-24 | 2012-02-01 | NV Bekaert SA | Régénérateur pour moteur à cycle thermique |
US20110314789A1 (en) * | 2009-03-24 | 2011-12-29 | Nv Bekaert Sa | Regenerator for a thermal cycle engine |
DE102011050368A1 (de) * | 2011-05-15 | 2012-11-15 | Webasto Ag | Verdampferanordnung |
US8637792B2 (en) | 2011-05-18 | 2014-01-28 | Prince Castle, LLC | Conveyor oven with adjustable air vents |
US11255538B2 (en) * | 2015-02-09 | 2022-02-22 | Gas Technology Institute | Radiant infrared gas burner |
DE102015110829B4 (de) * | 2015-07-06 | 2019-11-28 | Webasto SE | Poröses Brennstoffaufbereitungselement |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2050298A (en) * | 1934-04-25 | 1936-08-11 | Thos Firth & John Brown Ltd | Metal reducing method |
GB876435A (en) * | 1958-11-24 | 1961-08-30 | Du Pont | Polytetrafluoroethylene bearing and process for the production thereof |
US3262190A (en) * | 1961-07-10 | 1966-07-26 | Iit Res Inst | Method for the production of metallic heat transfer bodies |
US3291577A (en) * | 1963-09-12 | 1966-12-13 | Clevite Corp | Oxidation resistant material |
US3394213A (en) * | 1964-03-02 | 1968-07-23 | Roehr Prod Co Inc | Method of forming filaments |
US3490902A (en) * | 1965-04-13 | 1970-01-20 | Huyck Corp | Metal fiber reinforcement |
US3277564A (en) * | 1965-06-14 | 1966-10-11 | Roehr Prod Co Inc | Method of simultaneously forming a plurality of filaments |
US3469297A (en) * | 1966-04-20 | 1969-09-30 | Brunswick Corp | Porous metal structure |
JPS5033992A (fr) * | 1973-07-31 | 1975-04-02 | ||
GB1471138A (en) * | 1974-05-06 | 1977-04-21 | Atomic Energy Authority Uk | Supports for catalyst materials |
CA1103279A (fr) * | 1976-04-15 | 1981-06-16 | Carlino Panzera | Etancheites ceramiques poreuses, et methode de fabrication connexe |
BE850935A (fr) * | 1976-11-01 | 1977-05-16 | Textron Inc | Elements de filtre et leur fabrication |
JPS5554505A (en) * | 1978-10-19 | 1980-04-21 | Hitachi Powdered Metals Co Ltd | Member for sintering jig |
JPS5933009A (ja) * | 1982-08-17 | 1984-02-22 | Ishikawajima Harima Heavy Ind Co Ltd | 竪形圧延機の竪ロ−ル昇降装置 |
GB8405681D0 (en) * | 1984-03-05 | 1984-04-11 | Shell Int Research | Surface-combustion radiant burner |
-
1986
- 1986-11-05 EP EP86201928A patent/EP0227131B1/fr not_active Expired - Lifetime
- 1986-11-05 DE DE8686201928T patent/DE3671407D1/de not_active Expired - Lifetime
- 1986-11-14 US US06/930,496 patent/US4810587A/en not_active Expired - Lifetime
- 1986-11-28 JP JP61284117A patent/JP2593459B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US4810587A (en) | 1989-03-07 |
JP2593459B2 (ja) | 1997-03-26 |
EP0227131A1 (fr) | 1987-07-01 |
JPS62144942A (ja) | 1987-06-29 |
DE3671407D1 (de) | 1990-06-28 |
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